Effects of detonation instability and boundary layer on flame propagation behavior in millimeter-scale smooth tubes

Author:

Pan Zhenhua,Zhu Minhao,Zhang Penggang

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference48 articles.

1. Detonative propulsion;Wolański;Proc. Combust. Inst.,2013

2. Investigation of pulse detonation combustors-axial turbine system;Anand;Aerosp. Sci. Technol.,2019

3. Effects of the combustor width on propagation characteristics of rotating detonation waves;Wang;Aerosp. Sci. Technol.,2020

4. Experimental and numerical investigation on flame propagation and transition to detonation in curved channel;Pan;Aerosp. Sci. Technol.,2020

5. Initial stages of a spherical detonation directly initiated by a laser spark;Klimkin;Combust. Flame,1973

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1. Experimental investigation of detonation decay in rough narrow channels;International Journal of Hydrogen Energy;2024-01

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